View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 27610U 26018.36411172 +.00000000 +00000-0 +44408-4 0 00005
2 27610 64.5576 235.9672 0268018 116.8323 52.8340 14.29483808 03
| Epoch (UTC): | 18 January 2026 08:44:19 |
| Eccentricity: | 0.0268018 |
| inclination: | 64.5576° |
| perigee height: | 601 km |
| apogee height: | 986 km |
| right ascension of ascending node: | 235.9672° |
| argument of perigee: | 116.8323° |
| revolutions per day: | 14.29483808 |
| mean anomaly at epoch: | 52.8340° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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